FENGYUN 1C DEB, 30525
Orbit data source: Space-Track
FENGYUN 1C DEB, 30525 is space debris in SSO originally from a launch on Mon, 10 May 1999 UTC launched from the Taiyaun Space Center, China (TSC). Fengyun 1C debris stems from the Chinese weather satellite Fengyun-1C, which was intentionally destroyed by a Chinese anti-satellite missile in 2007. This event dramatically increased the amount of space debris, with thousands of trackable fragments posing hazards to satellites and human spaceflight. The Fengyun 1C debris cloud has become a focal point in discussions about space sustainability and the need for international regulations to prevent the creation of new debris.
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30525 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 FENGYUN 1C DEB
1 30525U 99025AJP 26095.58582044 .00001928 00000-0 20159-2 0 9997
2 30525 98.5977 331.8811 0293808 11.9357 348.8556 13.58988962946639Epoch: 2026-04-05T14:03Z
TLE epoch observation values (Epoch: 2026-04-05T14:03:34.886Z)
Latitude
-0.00005°
Longitude
-72.90337°
Altitude
828.591 km
Speed
7.545 km/s
True Right ascension
22h 07m 31s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:48:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,254.452 km
Perigee altitude
818.75 km
Semi-major axis
7,414.738 km
Eccentricity
0.02938
Inclination
98.5977°
RAAN
331.8811°
Arg. of periapsis
11.9357°
True anomaly
348.18059°
Mean anomaly
348.8556°
Eccentric anomaly
348.52058°
Mean motion
3.39938 °/min
Orbital period
105.9 mins
BSTAR
0.0020159
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Other satellites on launch #25 in the year 1999 (1999-05-10 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FENGYUN 1C DEB Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-06 03:02:29.152Z | 52.166° ENE | 2026-04-06 03:06:29.152Z | 89.736° E | 17.974° | 2026-04-06 03:10:29.152Z | 126.925° SE |
| 12 mins | 2026-04-06 04:46:29.152Z | 8.896° NNE | 2026-04-06 04:51:29.152Z | 300.889° NW | 44.264° | 2026-04-06 04:58:29.152Z | 201.821° SSW |
| 5 mins | 2026-04-06 06:33:29.152Z | 319.254° NNW | 2026-04-06 06:35:29.152Z | 300.341° NW | 14.065° | 2026-04-06 06:38:29.152Z | 274.391° WNW |
| 8 mins | 2026-04-06 14:56:29.152Z | 124.392° SE | 2026-04-06 14:59:29.152Z | 74.608° E | 31.417° | 2026-04-06 15:04:29.152Z | 3.856° NNE |
| 7 mins | 2026-04-06 16:41:29.152Z | 221.883° SW | 2026-04-06 16:44:29.152Z | 265.567° W | 23.23° | 2026-04-06 16:48:29.152Z | 317.543° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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